H130 technical information

H130 Falcon Aviation delivery

Introduction

The H130 is derived from Airbus’ Ecureuil family of light helicopters, which is renowned for its performance, reliability, safety, and multi-mission capability.

Technical description

Performance

Hover ceiling OGE @ MTOW, ISA
2,957 m
Hover ceiling IGE @ MTOW, ISA
3,429 m
Fast cruise speed @ MTOW
237 km/h
Max range @ fast cruise speed
606 km
Max endurance @ fast cruise speed
4 hr, 00 min
Flight envelope (temperature)
-40°C to ISA +35°C limited to 50°C
Max altitude flight
7,010 m

Dimensions

D-value
12.64 m
Rotor diameter
10.69 m
Cabin intern. volume (excluding pilot's area)
3.70 m³

Characteristics

Crew + passengers
1 pilot + 7 pax or 2 pilots + 5 pax
Max takeoff weight (MTOW)
2,500 kg
Max takeoff weight with external load
3,050 kg
Useful load
1,039 kg
Standard fuel tank capacity
425 kg
Engine type
Safran Helicopter Engines Arriel 2D
Takeoff power
710 kW / 952 shp

Configurations

Five or six seats

Passenger configuration

6-seats-H130-configuration

Seven seats

Passenger configuration

7-seats-H130-configuration

Documents

Overview brochures

Civil Range Brochure

Civil Range Brochure

Mission brochure

H130 infographic

Civil Range Brochure

Civil Range Brochure

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